- TCCAEASA 2026-37 · Time Limits / Maintenance Checks - Airworthiness Limitation Items - Amendment
Effective: 2026-08-06
- TCCAEASA 2026-06R1 · Landing Gear - Main Landing Gear Aft Door Mechanism - Lock Link Apex Pin/Bolt Fracture
Effective: 2026-07-16
- FAA AD 2026-11-06 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2026-07-09
The FAA is adopting a new airworthiness directive (AD) for all De Havilland Aircraft of Canada Limited Model DHC-8 airplanes. This AD was prompted by reports of cracked barrel nuts at the wing front s
- FAA AD 2026-08-07 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2026-06-03
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-401 and - 402 airplanes. This AD was prompted by multiple in-service reports of c
- TCCAEASA 2025-54R1 · Navigation - 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in Canadian airspace affected by 5G C-Band wireless signals
Effective: 2026-04-13
- TCCAEASA 2026-06 · Landing Gear - Main Landing Gear Aft Door Mechanism - Lock Link Apex Pin/Bolt Fracture
Effective: 2026-02-05
- TCCAEASA 2026-04 · Landing Gear - Main Landing Gear Premature Tire Failure
Effective: 2026-02-02
- TCCAEASA 2025-69 · Fuel System - Potential Fuel Leak in Dry-Bay - Missing Sealant
Effective: 2026-01-12
- TCCAEASA 2025-55 · Navigation - 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in Canadian airspace
Effective: 2025-11-12
- TCCAEASA 2025-54 · Navigation - 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in Canadian airspace affected by 5G C-Band wireless signals
Effective: 2025-11-12
- TCCAEASA 2025-52 · Navigation - 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in the contiguous United States of America (U.S.) airspace.
Effective: 2025-10-31
- FAA AD 2025-19-05 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2025-10-31
The FAA is superseding Airworthiness Directive (AD) 2019-16- 09, which applied to certain De Havilland Aircraft of Canada Limited Model DHC-8-400 series airplanes. AD 2019-16-09 required one-time insp
- TCCAEASA 2025-43 · Navigation - 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in the contiguous United States of America (U.S.) airspace
Effective: 2025-09-09
- TCCAEASA 2025-33 · Wing - Wing Access Panels with Un-trimmed Stiffeners and/or Reduced Thickness
Effective: 2025-07-07
- TCCAEASA 2025-19 · Stabilizers - Elevator Power Control Unit (PCU) Bracket and Elevator Front Spar Cracks
Effective: 2025-03-31
- FAA AD 2025-05-06 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2025-04-16
The FAA is superseding Airworthiness Directive (AD) 2022-01- 02, which applied to certain De Havilland Aircraft of Canada Limited Model DHC-8-400, -401, and -402 airplanes. AD 2022-01-02 required insp
- FAA AD 2024-22-07 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2024-12-31
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-401 and - 402 airplanes. This AD was prompted by a report of an in-flight event w
- FAA AD 2024-12-06 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2024-08-21
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-401 and - 402 airplanes. This AD was prompted by reports of moisture in the wing-
- FAA AD 2024-12-05 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2024-08-21
The FAA is superseding Airworthiness Directive (AD) 2021-25-12 and AD 2022-11-11, which applied to certain De Havilland Aircraft of Canada Limited Model DHC-8-401 and -402 airplanes. AD 2021-25-12 req
- FAA AD 2024-08-04 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2024-06-20
The FAA is adopting a new airworthiness directive (AD) for all De Havilland Aircraft of Canada Limited Model DHC-8-401 and -402 airplanes. This AD was prompted by a determination that new or more rest
- TCCAEASA 2024-10 · Flight Controls - Elevator Power Control Unit Bracket Cracks
Effective: 2024-03-08
- TCCAEASA 2020-51R2 · Nacelles/Pylons - Attachment Pin Corrosion
Effective: 2024-02-28
- FAA AD 2024-02-02 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2024-03-21
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-401 and - 402 airplanes. This AD was prompted by reports that the saddle washer (
- TCCAEASA 2024-01 · Landing Gear - Main Landing Gear - Brake Fuse/Shuttle Valve Assembly - Failure Caused by Assembly Error
Effective: 2024-01-12
- FAA AD 2023-16-05 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2023-09-25
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-401 and - 402 airplanes. This AD was prompted by reports of the main landing gear
- FAA AD 2023-07-06 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2023-06-20
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-401 and - 402 airplanes. This AD was prompted by reports of corrosion on the hori
- EASA 2021-0234R1 · Information Systems - Electronic Flight Bag Universal Serial Bus Receptacle - Modification
Effective: 2023-05-11
- FAA AD 2023-06-03 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2023-05-18
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-401 and - 402 airplanes. This AD was prompted by an investigation of incorrectly
- TCCAEASA 2023-22 · Landing Gear - Nose Landing Gear and Doors - Loss of Pivot Pin Retention Bolt
Effective: 2023-03-31
- FAA AD 2023-05-01 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2023-04-18
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-400 series airplanes. This AD was prompted by reports of flap power unit (FPU) pr
- FAA AD 2023-01-09 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2023-03-13
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-400 series airplanes. This AD was prompted by a report that electrical bonding ju
- FAA AD 2022-25-06 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2023-01-23
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-402 airplanes. This AD was prompted by an investigation that found that the actua
- TCCAEASA 2022-69 · Landing Gear - Alternate Extension System - Cam Assembly Failures
Effective: 2022-12-19
- TCCAEASA 2022-63 · Fuselage - Wing-to-Fuselage Joint - Moisture Ingress Between Front and Rear Spar Frame Segments
Effective: 2022-11-18
- FAA AD 2022-23-01 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2022-12-13
The FAA is superseding Airworthiness Directive (AD) 2020-04- 20, which applied to certain De Havilland Aircraft of Canada Limited Model DHC-8-400 series airplanes. AD 2020-04-20 required repetitive in
- TCCAEASA 2022-59 · Maintenance Requirements Manual, Part 2 Airworthiness Limitation Items - Introduction of New Section 7-00 - Candidate Certification Maintenance Requirements Limitations
Effective: 2022-10-28
- FAA AD 2022-17-04 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2022-11-01
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-400 series airplanes. This AD was prompted by reports of broken P-clamps on the p
- TCCAEASA 2022-52 · Flight Controls - Flap Power Unit - Pressure Switch Failures
Effective: 2022-09-02
- FAA AD 2022-13-08 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2022-08-10
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-401 and - 402 airplanes. This AD was prompted by reports of nose wheel steering (
- FAA AD 2022-11-14 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2022-06-21
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-401 and - 402 airplanes. This AD was prompted by reports that following a main la
- FAA AD 2022-11-11 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2022-07-08
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited (type certificate previously held by Bombardier, Inc.) Model DHC-8-401 and -402 airplanes. Th
- TCCAEASA 2022-29 · Landing Gear - Main Landing Gear (MLG) and Doors - Forward Door Linkage Sleeves Missing Greasing Grooves
Effective: 2022-05-30
- TCCAEASA 2022-21 · Stabilizers - Horizontal Stabilizer to Vertical Stabilizer Joint - Non-Conforming Saddle Washer (Radius Filler)
Effective: 2022-04-25
- FAA AD 2022-06-15 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2022-05-10
The FAA is adopting a new airworthiness directive (AD) for all De Havilland Aircraft of Canada Limited Model DHC-8-401 and -402 airplanes. This AD was prompted by reports of bleed air leaks in the win
- TCCAEASA 2022-12 · Landing Gear - Lubrication of Main Landing Gear
Effective: 2022-03-22
- TCCAEASA 2022-09 · Air Conditioning - Avionics Cooling - Integrated Flight Cabinet Failure Due to High Temperatures
Effective: 2022-03-04
- FAA AD 2022-03-02 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2022-03-17
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-401 and - 402 airplanes. This AD was prompted by reports of a possible hard conta
- TCCAEASA 2022-02 · Stabilizers - Horizontal Stabilizer Lower Centre Skin Panel - Corrosion Damage
Effective: 2022-02-01
- FAA AD 2022-01-02 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2022-03-03
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-400, -401, and -402 airplanes. This AD was prompted by a report that the epoxy pr
- FAA AD 2021-25-12 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2022-01-05
The FAA is superseding Airworthiness Directive (AD) 2017-19- 09, which applied to certain De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Model DHC-8-400
- FAA AD 2021-23-02 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2022-01-05
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-401 and - 402 airplanes. This AD was prompted by reports of loss of hydraulic flu
- FAA AD 2021-23-03 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2021-12-06
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-400, -401, and -402 airplanes. This AD was prompted by a report of cracking found
- EASA 2021-0234 · Information Systems - Electronic Flight Bag Universal Serial Bus Receptacle - Modification
Effective: 2021-10-28
- FAA AD 2021-19-11 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2021-11-18
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-102, -103, and -106 airplanes; Model DHC-8-201 and -202 airplanes; Model DHC-8- 3
- TCCAEASA 2009-29R4 · Nose Landing Gear - Loss of Pivot Pin Retention Bolt
Effective: 2021-10-04
- TCCAEASA 2009-29R3 · Nose Landing Gear - Loss of Pivot Pin Retention Bolt
Effective: 2021-09-15
- TCCAEASA 2021-28 · Landing Gear - Nose Wheel Steering Hydraulic Motor - Potential Jam Due to Wear
Effective: 2021-08-12
- FAA AD 2021-12-02 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2021-07-20
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-400 series airplanes. This AD was prompted by a report that a number of nacelle A
- FAA AD 2021-11-04 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2021-07-09
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-400, -401, and -402 airplanes. This AD was prompted by a report of main landing g
- FAA AD 2021-10-13 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2021-07-01
The FAA is superseding Airworthiness Directive (AD) 2015-17- 08, which applied to certain Bombardier, Inc. Model DHC-8-400 series airplanes. AD 2015-17-08 required installing new cable assemblies with
- TCCAEASA 2021-12 · Fire Protection System - Main Landing Gear Primary Zone Advanced Pneumatic Detector Chafing Damage
Effective: 2021-04-06
- TCCAEASA 2021-11 · Pneumatic System - Wing Check Valve Bleed Air Leak - Replacement
Effective: 2021-03-30
- TCCAEASA 2021-08 · Fuel System - Fuel Terminal - High Level Sensor Terminal Screw in Contact with Access Panel
Effective: 2021-03-16
- TCCAEASA 2020-51R1 · Nacelles/Pylons - Attachment Pin Corrosion
Effective: 2021-02-25
- TCCAEASA 2020-06R1 · Standard Practices/Structures - Introduction of Barrel Nut Inspections
Effective: 2021-01-12
- TCCAEASA 2020-51 · Nacelles/Pylons - Attachment Pin Corrosion
Effective: 2020-12-01
- TCCAEASA 2020-43 · Landing Gear - Main Landing Gear Drag Strut - Longitudinal Cracking
Effective: 2020-10-22
- TCCAEASA 2020-39 · Nacelles/Pylons - Main Landing Gear Side Brace Fitting to A-frame Joint - Fastener Holes Not Cold-worked
Effective: 2020-10-15
- FAA AD 2020-21-03 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2020-11-18
The FAA is superseding Airworthiness Directive (AD) 2015-14- 01, which applied to certain Bombardier, Inc., Model DHC-8-400 series airplanes. AD 2015-14-01 required a detailed inspection for loose bol
- TCCAEASA 2020-34 · Flight Controls - Rudder Actuator Bracket - Cracked or Missing Nuts
Effective: 2020-10-07
- TCCAEASA 2020-28 · Landing Gear - Nose Wheel Steering System - Un-Commanded Nose Wheel Deviation
Effective: 2020-08-28
- FAA AD 2020-11-13 · July 14, 2020 Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2020-07-14
The FAA is superseding Airworthiness Directive (AD) 2010-23- 04, which applied to all De Havilland Aircraft of Canada Limited Model DHC-8-400 series airplanes. AD 2010-23-04 required repetitive detail
- FAA AD 2020-09-12 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2020-06-24
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-400 series airplanes. This AD was prompted by a report that certain elevator powe
- TCCAEASA 2017-04R3 · Fuel System - Corrosion and Wear of Hydraflow Couplings and Sleeves, Fuel Tube End Ferrules, and Fuel Component End Ferrules
Effective: 2020-04-02
- FAA AD 2020-04-20 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2020-05-04
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-400 series airplanes. This AD was prompted by reports of wear on fuel couplings,
- TCCAEASA 2020-06 · Standard Practices/Structures - Introduction of Barrel Nut Inspections
Effective: 2020-03-16
- FAA AD 2020-02-10 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2020-03-12
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-400 series airplanes. This AD was prompted by a report of a quality escape in the
- TCCAEASA 2020-01 · Fuel System - Non-Conforming Installation of Electrical Bonding Jumpers
Effective: 2020-01-15
- FAA AD 2019-24-12 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2020-02-03
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-401 and - 402 airplanes. This AD was prompted by a report that certain fuselages
- FAA AD 2019-22-11 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2020-01-09
The FAA is superseding Airworthiness Directive (AD) 2009-09- 02, which applied to certain Bombardier, Inc., Model DHC-8-400 series airplanes. AD 2009-09-02 required repetitive inspections for damage o
- TCCAEASA 2018-01R2 · Landing Gear - Nose Landing Gear Drag Strut Lock Link Wear
Effective: 2019-12-02
- TCCAEASA 2019-36 · Stabilizers - Elevator Power Control Unit (PCU) Arm Fittings Insufficient Fillet Radius
Effective: 2019-10-25
- FAA AD 2019-20-09 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2019-11-27
The FAA is superseding Airworthiness Directive (AD) 2011-18- 15, which applied to certain De Havilland Aircraft of Canada Limited Model DHC-8-400 series airplanes. AD 2011-18-15 required initial and r
- TCCAEASA 2017-05R2 · Fuel System - Motive Flow Line Fouling, Motive Flow Line and Pressure Relief Line Broken P-Clamps, and Vent Line TeflonTM Sleeve Installation
Effective: 2019-10-01
- FAA AD 2019-18-05 · Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Effective: 2019-10-31
The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Model DHC-8-400 series airplanes. This
- FAA AD 2019-16-09 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2019-10-09
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model DHC-8-400 series airplanes. This AD was prompted by reports of cracked elevator power control unit (PCU) brac
- FAA AD 2019-15-09 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2019-09-19
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model DHC-8-400 series airplanes. This AD was prompted by a report of a cracked outboard spoiler actuator mounting
- TCCAEASA 2014-08R1 · Doors - Translating Doors Loose Bolts
Effective: 2019-08-01
- TCCAEASA 2010-30R2 · Cracking of the Nacelle Attachment Fitting(s)
Effective: 2019-08-01
- FAA AD 2019-12-17 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2019-08-12
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model DHC-8-102, -103, and -106 airplanes; Model DHC-8-200 series airplanes; and Model DHC-8-300 series airplanes.
- TCCAEASA 2019-13 · Fire Detection System - Contamination of the sensor contacts for Advanced Pneumatic Detectors (APD) System
Effective: 2019-04-15
- TCCAEASA 2019-06 · Fuselage - Non-Conforming Keel Tension Fittings and Stringer End Fittings
Effective: 2019-03-01
- FAA AD 2018-23-04 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2019-03-15
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model DHC-8-102, -103, and -106 airplanes; Model DHC- 8-200 series airplanes; and Model DHC-8-300 series airplanes. Thi
- EASA 2018-0259R1 · Information Systems - Electronic Flight Bag Universal Serial Bus Receptacle - Modification
Effective: 2019-02-07
- TCCAEASA 2009-11R3 · Failure of the Main Landing Gear Stabilizer Braces
Effective: 2019-02-01
- TCCAEASA 2018-01R1 · Landing Gear - Nose Landing Gear Drag Strut Lock Link Wear
Effective: 2019-01-28
- TCCAEASA 2011-24R1 · Wings - Wing to Fuselage Attachment Joints - Barrel Nut Cracking
Effective: 2019-01-28
- TCCAEASA 2018-34 · Flight Controls - Elevator Power Control Unit Bracket Cracking
Effective: 2018-12-20
- EASA 2018-0259 · Information Systems - Electronic Flight Bag Universal Serial Bus Receptacle - Modification
Effective: 2018-11-30
- FAA AD 2018-20-11 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2018-11-23
The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to certain Bombardier, Inc., Model DHC-8-300 series airplanes. As published, a service inf
- TCCAEASA 2018-30 · Stabilizers - Elevator - Spring Tab - Mass Balance Hinge Arm Fracture
Effective: 2018-11-12
- TCCAEASA 2018-21R1 · Wings - Cracked Spoiler Actuator Bracket
Effective: 2018-10-25
- FAA 2018-23031 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2018-11-28
We are superseding Airworthiness Directive (AD) 2016-24-03, which applied to certain Bombardier, Inc., Model DHC-8-400 series airplanes. AD 2016-24-03 required repetitive detailed inspections of barre
- FAA AD 2018-20-18 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2018-11-20
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model DHC-8-400 series airplanes. This AD was prompted by a report of uncommanded deployment of the ground spoilers whe
- TCCAEASA 2017-04R2 · Fuel System - Corrosion and Wear of Hydraflow Couplings and Sleeves, Fuel Tube End Ferrules, and Fuel Component End Ferrules
Effective: 2018-10-03
- FAA AD 2018-17-17 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2018-10-02
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model DHC-8-400 series airplanes. This AD was prompted by reports of arcing and smoke emanating from the windshields. T
- FAA AD 2018-17-09 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2018-09-25
We are superseding Airworthiness Directive (AD) 2014-05-28, which applied to certain Bombardier, Inc., Model DHC-8-400 series airplanes. AD 2014-05-28 required revising the maintenance or inspection p
- TCCAEASA 2018-21 · Wings - Cracked Spoiler Actuator Bracket
Effective: 2018-08-07
- TCCAEASA 2009-11R2 · Main Landing Gear - Main Landing Gear Stabilizer Braces - Inspection
Effective: 2018-06-07
- TCCAEASA 2018-09 · Furnishings - Forward Lavatory Door Hinge Flexing
Effective: 2018-03-15
- FAA AD 2018-02-16 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2018-03-05
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model DHC-8-400 series airplanes. This AD was prompted by reports that operation of fuselage doors was interrupted due
- TCCAEASA 2018-01 · Landing Gear - Nose Landing Gear Drag Strut Lock Link Wear
Effective: 2018-01-15
- TCCAEASA 2017-35 · Flight Controls - Power Lever Module - Introduction of Operational Check of Ground Spoiler Switches
Effective: 2017-12-01
- TCCAEASA 2009-11R1 · Main Landing Gear - Main Landing Gear Stabilizer Braces - Inspection
Effective: 2017-11-24
- FAA AD 2017-23-01 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2017-12-19
We are superseding Airworthiness Directive (AD) 2016-13-14, which applied to certain Bombardier, Inc., Model DHC-8-400 series airplanes. AD 2016-13-14 required an inspection to determine if certain le
- FAA AD 2017-20-07 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2017-11-06
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model DHC-8-400 series airplanes. This AD was prompted by the failure of the fire control amplifier (FCA), which was li
- FAA AD 2017-19-27 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2017-11-01
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model DHC-8-401 and -402 airplanes. This AD was prompted by the discovery of cracking on two test spoiler power control
- TCCAEASA 2017-05R1 · Fuel System - Motive Flow Line Fouling and Motive Flow Line and Pressure Relief Line Broken P-Clamps
Effective: 2017-09-22
- FAA AD 2017-19-09 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2017-10-24
We are superseding Airworthiness Directive (AD) 2014-25-01, which applied to certain Bombardier, Inc., Model DHC-8-400 series airplanes. AD 2014-25-01 required modifying the nose landing gear (NLG) tr
- TCCAEASA 2017-30 · Doors - Forward Right Hand Type I Emergency Exit Hardware Corrosion
Effective: 2017-09-06
- FAA AD 2017-17-02 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2017-09-25
We are superseding Airworthiness Directive (AD) 2014-20-09, which applied to certain Bombardier, Inc., Model DHC-8-400 series airplanes. AD 2014-20-09 required an inspection for missing clamps that ar
- FAA AD 2017-15-11 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2017-09-05
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes. This AD was prompted by reports of undamped ma
- TCCAEASA 2017-25 · Windows - Windshield Cracking
Effective: 2017-08-01
- FAA AD 2017-14-02 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2017-08-10
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model DHC-8-401 and DHC-8-402 airplanes. This AD was prompted by a report that a pilot was unable to move the rudder pe
- TCCAEASA 2017-21R1 · Engine Ignition - Loss of #2 Engine Auto Relight Function
Effective: 2017-06-29
- TCCAEASA 2015-13R1 · Stabilizers - Cracked Barrel Nut at the Horizontal Stabilizer to Vertical Stabilizer Attachment Joint
Effective: 2017-06-27
- TCCAEASA 2014-45R3 · Nacelle - A-Frame Structure - Insufficient Fillet Radius and Fouling with Main Landing Gear Stabilizer Brace and the Electrical Wiring Harnesses
Effective: 2017-06-19
- TCCAEASA 2017-18 · Windows - Windshield Cracking - Inspection
Effective: 2017-05-30
- TCCAEASA 2017-04R1 · Fuel System - Corrosion and Wear of Hydraflow Couplings and Sleeves, Fuel Tube End Ferrules, and Fuel Component End Ferrules
Effective: 2017-05-30
- FAA AD 2017-09-11 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2017-06-29
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of interruptions in the airstair door operation. This
- TCCAEASA 2017-15 · Landing Gear - Main Landing Gear Up-Lock Assembly Latch Wear - Introduction of One-Star Certification Maintenance Requirement Task 323100-102
Effective: 2017-05-17
- TCCAEASA 2016-36R1 · Landing Gear - Main Landing Gear Retraction Actuator Rod-End Failure
Effective: 2017-05-17
- FAA AD 2017-08-02 · Airworthiness Directives; Bombardier, Inc., Airplanes
Effective: 2017-05-17
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model DHC-8-102, -103, and -106 airplanes; and Model DHC-8-200 and DHC-8-300 series airplanes. This AD was prompted by
- TCCAEASA 2014-45R2 · Nacelle - A-Frame Structure - Insufficient Fillet Radius and Fouling with Main Landing Gear Stabilizer Brace and the Electrical Wiring Harnesses
Effective: 2017-03-30
- FAA AD 2017-06-10 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2017-05-01
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of interior emergency lights remaining "ON" following
- TCCAEASA 2016-31R1 · Landing Gear - Dynamic Response of Main Landing Gear System to External Loads
Effective: 2017-03-27
- FAA AD 2017-05-11 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2017-04-17
We are superseding Airworthiness Directive (AD) 2012-08-11 for certain Bombardier, Inc. Model DHC-8-400 series airplanes. AD 2012-08- 11 required repetitive inspections for defects and damage of the r
- TCCAEASA 2017-05 · Fuel System - Motive Flow Line Fouling and Motive Flow Line and Pressure Relief Line Broken P-Clamps
Effective: 2017-01-30
- TCCAEASA 2013-15R2 · Propellers - In-flight Operation of Propeller in Beta Range
Effective: 2017-01-27
- TCCAEASA 2017-04 · Fuel System - Corrosion and Wear of Hydraflow Couplings and Sleeves, Fuel Tube End Ferrules, and Fuel Component End Ferrules
Effective: 2017-01-26
- TCCAEASA 2015-07R2 · Flight Control System - Cracking of the Spoiler Power Control Unit
Effective: 2016-12-20
- FAA AD 2016-24-04 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2017-01-17
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by a determination by the manufacturer that shims might not have
- TCCAEASA 2009-29R2 · Nose Landing Gear - Loss of Pivot Pin Retention Bolt
Effective: 2016-12-12
- FAA AD 2016-24-06 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2017-01-12
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, and -106 airplanes, Model DHC- 8-200 series airplanes, and Model DHC-8-300 series airplanes. This
- FAA AD 2016-24-03 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2017-01-12
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of cracked and corroded barrel nuts found at the mid-s
- TCCAEASA 2016-36 · Landing Gear - Main Landing Gear Retraction Actuator Rod-End Failure
Effective: 2016-11-29
- FAA AD 2016-24-01 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2016-12-30
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, and -106 airplanes; and Model DHC-8-200 and -300 series airplanes. This AD was prompted by a repo
- FAA AD 2016-22-03 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2016-11-30
We are adopting a new airworthiness directive (AD) for all Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by a revision by the manufacturer to the Certification Maintenance Re
- TCCAEASA 2015-07R1 · Flight Control System - Cracking of the Spoiler Power Control Unit
Effective: 2016-10-21
- TCCAEASA 2016-31 · Landing Gear - Dynamic Response of Main Landing Gear System to External Loads
Effective: 2016-09-30
- FAA AD 2016-19-11 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2016-11-02
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by a malfunctioning No. 2 engine intake heater with corrosion on
- TCCAEASA 2014-45R1 · Nacelle - A-Frame Structure - Insufficient Fillet Radius and Fouling with Main Landing Gear Stabilizer Brace and the Electrical Wiring Harnesses
Effective: 2016-09-22
- TCCAEASA 2016-27 · Equipment and Furnishings - Instrument Panel - Pilot and Co-pilot Wiring Shroud Inspection and Modification
Effective: 2016-09-16
- TCCAEASA 2016-25 · Fire Protection - Inadvertent Discharge of Multiple Fire Extinguishing Bottles
Effective: 2016-08-31
- FAA AD 2016-16-15 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2016-09-23
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400, -401, and -402 airplanes. This AD was prompted by reports of chafing damage due to insufficient clearan
- TCCAEASA 2013-16R1 · Electrical Power - Alternating Current (AC) Feeder Cable Clamps Omitted
Effective: 2016-07-14
- FAA AD 2016-13-14 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2016-07-20
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD requires an inspection to determine if certain left and right main landing gea
- TCCAEASA 2016-16R1 · Landing Gear - Main Landing Gear - Retract Actuator Rod End Cracking
Effective: 2016-06-28
- TCCAEASA 2016-18 · Doors - Operation of Translating Door Restricted due to Bearing Corrosion
Effective: 2016-06-14
- TCCAEASA 2016-16 · Landing Gear - Main Landing Gear - Retract Actuator Rod End Cracking
Effective: 2016-05-23
- FAA AD 2016-10-07 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2016-06-23
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes. This AD was prompted by a report of a pilot com
- TCCAEASA 2016-12 · Lights - Emergency Lighting - Heat Damage to Emergency Lights Power Supply Negative Interlock and Ground Wires
Effective: 2016-04-29
- FAA AD 2016-01-09 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2016-02-25
We are adopting a new airworthiness directive (AD) for certain Bombardier Model DHC-8-400 series airplanes. This AD was prompted by a report of several cracks found on the forward passenger airstair d
- TCCAEASA 2016-04 · Ice and Rain Protection - Pitot and Static System - Pitot Probe Heater Circuit Breaker Tripping During Adverse Environmental Conditions
Effective: 2016-01-19
- FAA AD 2015-21-02 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2015-11-24
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes. This AD was prompted by reports of un-annunciat
- FAA AD 2015-19-13 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2015-11-03
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of inadvertent deployment of a single outboard spoiler
- FAA AD 2015-17-25 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2015-10-07
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of chafing of the fuel lines due to contact with the s
- FAA AD 2015-17-03 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2015-10-07
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400, -401, and -402 airplanes. This AD was prompted by a report of a main landing gear (MLG) parking brake b
- FAA AD 2015-17-08 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2015-09-29
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by an in-service report of an uncommanded and unannunciated nose
- TCCAEASA 2015-24 · Ice and Rain Protection - Engine Air Intake Heater Thermostats Corrosion
Effective: 2015-08-18
- TCCAEASA 2015-22 · Fuselage - Missing Shims Between Longerons and Longeron Joint Fittings
Effective: 2015-07-29
- FAA AD 2015-15-07 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2015-08-12
We are superseding Airworthiness Directive (AD) 2015-10-01 for certain Bombardier, Inc. Model DHC-8-400 series airplanes. AD 2015-10- 01 required inspection for correct assembly of the main landing ge
- FAA AD 2015-14-03 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2015-08-21
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes. This AD was prompted by fuel system reviews con
- FAA AD 2015-14-01 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2015-08-11
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by a report of loose bolts that are intended to secure the transl
- FAA AD 2015-13-02 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2015-07-31
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of corrosion in the low-rate discharge tubes of the fi
- TCCAEASA 2015-13 · Stabilizers - Cracked Barrel Nut at the Horizontal Stabilizer to Vertical Stabilizer Attachment Joint
Effective: 2015-06-12
- FAA AD 2015-10-01 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2015-07-14
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of hydraulic fluid loss from the reservoir of the main
- TCCAEASA 2011-14R1 · Landing Gear - Main Landing Gear Retraction Actuator - Retract Port Flexible Hose Failure
Effective: 2015-05-08
- FAA AD 2015-08-03 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2015-05-26
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by a report that during production, an incorrect clevis was used,
- TCCAEASA 2015-07 · Flight Control System - Cracking of the Spoiler Power Control Unit
Effective: 2015-04-15
- TCCAEASA 2012-29R1 · Electrical Power - Alternating Current Generator Mounting Plate Corrosion
Effective: 2015-04-15
- FAA AD 2015-04-08 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2015-04-27
We are superseding Airworthiness Directive (AD) 2014-06-08 for certain Bombardier, Inc. Model DHC-8-100, -200, and -300 series airplanes. AD 2014-06-08 required repetitive functional checks of the nos
- FAA AD 2015-02-25 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2015-03-17
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by fuel system reviews conducted by the manufacturer. This AD req
- FAA AD 2015-02-12 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2015-03-06
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of two in-service incidents where one side of the main
- TCCAEASA 2015-02 · Doors - Airstair Door Jammed due to Deformed Handrail Stowage Hardware
Effective: 2015-01-28
- TCCAEASA 2014-45 · Nacelle - A-Frame Structure - Insufficient Fillet Radius and Fouling with Main Landing Gear Stabilizer Brace and the Electrical Wiring Harnesses
Effective: 2015-01-05
- TCCAEASA 2014-43 · Propeller Overspeed Governor - Incorporation of New Certification Maintenance Requirement (CMR) Task
Effective: 2014-12-15
- FAA AD 2014-25-01 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2015-01-16
We are superseding Airworthiness Directive (AD) 2010-13-04 for certain Bombardier, Inc. Model DHC-8-400 series airplanes. AD 2010-13- 04 required modifying the nose landing gear (NLG) trailing arm. Th
- FAA AD 2014-23-14 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2014-12-31
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of swing arm assemblies of engine fuel feed ejector pu
- TCCAEASA 2014-31R2 · Electrical Power - Generator Undervoltage
Effective: 2014-11-17
- TCCAEASA 2014-31R1 · Electrical Power - Generator Undervoltage
Effective: 2014-10-30
- FAA AD 2014-20-09 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2014-11-07
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of missing clamps that are required to provide positiv
- FAA AD 2014-19-02 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2014-10-24
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400, -401, and -402 airplanes. This AD was prompted by reports of rudder bearings falling out of the fore ru
- FAA AD 2013-15-06 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2014-10-20
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, -106, -201, -202, -301, -311, and --315 airplanes. This AD was prompted by reports of dual altern
- TCCAEASA 2014-31 · Electrical Power - Generator Undervoltage
Effective: 2014-09-08
- FAA AD 2014-16-07 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2014-09-23
We are superseding Airworthiness Directive (AD) 2011-15-09 for certain Bombardier, Inc. Model DHC-8-400, -401, and -402 airplanes. AD 2011-15-09 required repetitive inspections for proper operation of
- FAA AD 2014-15-20 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2014-09-19
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of failure of the high pressure shutoff valves (HPSOVs
- TCCAEASA 2014-03R1 · Direct Current Starter/Generator - Terminal-Block Missing Insulating Sleeves
Effective: 2014-08-07
- FAA AD 2014-15-07 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2014-09-02
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes. This AD was prompted by reports of a fractured
- TCCAEASA 2014-22 · Flight Controls - Outboard Spoiler Power Control Unit (PCU) - Inadvertent Spoiler Deployment
Effective: 2014-07-22
- FAA AD 2014-13-18 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2014-08-19
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model DHC-8-102, -103, and -106 airplanes; and DHC-8- 200 and DHC-8-300 series airplanes. This AD was prompted by a rep
- TCCAEASA 2014-18 · Main Landing Gear - Improperly Stowed Parking Brake Hand Pump Lever in Right Hand Side Nacelle
Effective: 2014-06-20
- TCCAEASA 2014-15 · Hydraulic Power - Main Landing Gear Alternate Extension System Reservoir - Leakage due to Incorrect Lid Assembly
Effective: 2014-06-12
- FAA AD 2014-05-28 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2014-05-08
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of excessive wear on the lower latch surface of the ma
- FAA AD 2014-06-08 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2014-04-14
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8 airplanes. This AD requires repetitive functional checks of the nose and main landing gear, and corrective a
- FAA AD 2014-05-17 · Airworthiness Directives; Bombardier Inc., Airplanes
Effective: 2014-05-02
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes. This AD was prompted by results from fuel syste
- FAA AD 2014-05-18 · Airworthiness Directives; Bombardier, Inc.
Effective: 2014-04-22
We are adopting a new airworthiness directive (AD) for all Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by a report that a batch of main landing gear (MLG) door actuators wi
- FAA AD 2014-03-04 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2014-04-09
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by a report of a translating door handle jamming during opening o
- TCCAEASA 2014-11 · Landing Gear - False Emergency Downlock Indication
Effective: 2014-02-17
- TCCAEASA 2014-08 · Forward Translating Door - Loose Bolts
Effective: 2014-02-17
- TCCAEASA 2014-06 · Fire Protection System - Tube Corrosion - Integrity Check / Replacement
Effective: 2014-01-22
- TCCAEASA 2014-03 · Direct Current Starter/Generator - Terminal-Block Missing Insulating Sleeves
Effective: 2014-01-15
- TCCAEASA 2013-20R1 · Forward Passenger Door - Cracking of the Airstair Step Assembly
Effective: 2014-01-06
- TCCAEASA 2013-40 · Incorrect Installation of the Main Landing Gear Emergency Release Clevis
Effective: 2013-12-11
- TCCAEASA 2013-15R1 · In-flight Operation of Propeller in Beta Range
Effective: 2013-12-09
- TCCAEASA 2013-38 · Design Deficiency of the Nose Wheel Steering Control Unit
Effective: 2013-11-29
- TCCAEASA 2013-35 · Engine Fuel Feed Ejector Pump Swing Arm Assembly Failure
Effective: 2013-11-25
- TCCAEASA 2013-36 · Auto-Ignition System - Incorrect Wire Installation
Effective: 2013-11-21
- TCCAEASA 2013-34 · Flight Controls - Fore Rudder Bearing Wear in Hinge Assembly - Inspection / Rectification
Effective: 2013-11-08
- FAA AD 2013-22-09 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2013-12-05
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400, -401, and -402 airplanes. This AD was prompted by reports of movement of the rudder pedals being impede
- FAA AD 2013-22-04 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2013-12-05
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, and -106 airplanes; and Model DHC-8-200, -300, and -400 series airplanes. This AD was prompted by
- TCCAEASA 2013-32 · Fuel System Safety - Non-Compliant Refuel Control Solenoid Valve Fitting
Effective: 2013-10-10
- TCCAEASA 2013-27 · Ice Protection System - Inoperative Timer and Monitor Unit
Effective: 2013-09-30
- FAA AD 2013-16-25 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2013-10-04
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of advance pneumatic detectors (APDs) for engine fire/
- FAA AD 2013-16-12 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2013-09-24
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, and -106 airplanes. This AD was prompted by a report of cracking in a lower longeron in a nacelle
- TCCAEASA 2009-29R1 · Nose Landing Gear - Loss of Pivot Pin Retention Bolt
Effective: 2013-08-19
- FAA AD 2013-14-09 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2013-09-10
We are superseding airworthiness directive (AD) 2012-14-04 for certain Bombardier, Inc. Model DHC-8-100, -200, and -300 series airplanes. AD 2012-14-04 required replacing certain parking brake accumul
- TCCAEASA 2013-19 · Main Landing Gear Stabilizer Brace - Over-Torque and Insufficient Greasing of Lock Link Apex Joint
Effective: 2013-08-05
- TCCAEASA 2013-20 · Forward Passenger Door - Cracking of the Airstair Step Assembly
Effective: 2013-07-26
- FAA AD 2013-13-17 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2013-08-26
We are superseding airworthiness directive (AD) 2011-13-08 for certain Bombardier, Inc. Model DHC-8-400 series airplanes. AD 2011-13- 08 required a free-play check for excessive free-play of the shaft
- TCCAEASA 2007-32R2 · Fuel System Safety - Introduction of Maintenance Tasks
Effective: 2013-07-01
- FAA AD 2013-09-04 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2013-08-02
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of chafing found on the main landing gear (MLG) yoke.
- TCCAEASA 2013-17R1 · Fractured Wing-to-Fuselage Strut Attachment Joint Bolt
Effective: 2013-06-28
- TCCAEASA 2013-16 · AC Feeder Cables not Clamped to Hydraulic Lines - Inspection / Rectification
Effective: 2013-06-19
- TCCAEASA 2013-15 · In-Flight Operation of Propeller in Beta Range
Effective: 2013-06-19
- TCCAEASA 2013-09R1 · Fuel System - Insufficient Clearance Between Fuel Line and Structure
Effective: 2013-06-03
- TCCAEASA 2011-01R2 · Main Landing Gear Alternate Extension System - Cam Mechanism not in Normal Rested Position
Effective: 2013-05-21
- TCCAEASA 2013-09 · Fuel System - Insufficient Clearance Between Fuel Line and Structure
Effective: 2013-04-11
- TCCAEASA 2013-07 · Fuel System Safety - Introduction of Design changes
Effective: 2013-03-07
- TCCAEASA 2012-01R1 · Beta Warning Horn System Failure
Effective: 2013-03-07
- TCCAEASA 2007-32R1 · Fuel System Safety - Introduction of Maintenance Tasks
Effective: 2013-03-07
- FAA AD 2013-04-07 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2013-04-09
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes. This AD was prompted by reports of the loss of
- TCCAEASA 2012-33 · In-Flight Operation of Propellers In Beta Range
Effective: 2012-12-17
- TCCAEASA 2012-07R1 · Cockpit "Engine Fire, Check Fire Detect" Warning and "FUEL OFF" Handle Lights Failure to Reset
Effective: 2012-12-12
- TCCAEASA 2012-29 · AC Generator Mounting Plate Corrosion
Effective: 2012-12-06
- TCCAEASA 2012-28R1 · Main Landing Gear Door Actuator Scraper Incorrect Installation
Effective: 2012-12-03
- TCCAEASA 2012-28 · Main Landing Gear Door Actuator Scraper Incorrect Installation
Effective: 2012-11-21
- FAA AD 2012-22-07 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2012-12-14
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400, -401, and -402 airplanes. This AD was prompted by reports of an in-service incident where the propeller
- TCCAEASA 2012-27 · Cracking of the Nacelle Lower Longeron
Effective: 2012-11-06
- FAA AD 2012-21-12 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2012-12-04
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by cases of on-ground failure of the screw cap or end cap of hydr
- TCCAEASA 2012-02R1 · Rudder Control System - Seizure of the Rudder Feel Trim Unit
Effective: 2012-10-22
- FAA AD 2012-20-08 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2012-11-21
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of alternating current (AC) generator failures in-serv
- FAA AD 2012-20-09 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2012-11-20
We are superseding an existing airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. That AD currently requires a modification to trim the edge of the bumper plat
- FAA AD 2012-20-04 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2012-11-14
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of chafing between the wire harness along the wing lea
- FAA AD 2012-18-15 · Airworthiness Directives; Bombardier Inc. Airplanes
Effective: 2012-10-22
We are adopting a new airworthiness directive (AD) for certain Bombardier Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports that the automatic de-icing mode became unavailable due
- TCCAEASA 2012-25 · Electrical Power - AC Wiring Harness Chafing on Centre Wing Lower Flap Shroud
Effective: 2012-08-30
- FAA AD 2012-16-10 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2012-09-18
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by chafing on high pressure fuel lines due to improper installati
- FAA AD 2012-15-16 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2012-09-12
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8 series airplanes. This AD was prompted by reports that various pushrods had been manufactured with tubes hav
- FAA AD 2012-14-04 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2012-08-27
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-100, DHC-8-200, and DHC-8-300 series airplanes. This AD was prompted by reports of hydraulic accumulator scr
- TCCAEASA 2012-21 · Main Landing Gear Up-lock Wear
Effective: 2012-07-02
- FAA AD 2012-12-16 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2012-07-30
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of cracking of certain fuel access panels of the outer
- TCCAEASA 2010-28R1 · Elevator Power Control Unit - Shaft (Tailstock) Swaged Bearing Wear - Replacement
Effective: 2012-06-13
- TCCAEASA 2012-17 · Aft Entry & Aft Service Doors - Translating Door Handle Jamming
Effective: 2012-05-25
- TCCAEASA 2011-29R1 · Hydraulic Accumulators - Screw Cap/End Cap Failure
Effective: 2012-05-25
- TCCAEASA 2012-15 · Chafing of the Nacelle Fire Detection Wire on the Main Landing Gear Yoke
Effective: 2012-05-03
- FAA AD 2012-08-11 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2012-05-29
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by test reports that showed that failure of a retract port flexib
- FAA AD 2012-06-05 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2012-04-27
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by a report of the inability to open the airstair door while on t
- FAA AD 2012-06-04 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2012-04-25
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of difficulties in opening the airstair door. This AD
- FAA AD 2012-05-07 · Airworthiness Directives; Bombardier, Inc.
Effective: 2012-04-04
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, and -106 airplanes. This AD requires a general visual inspection for chamfer of the upper edge of
- FAA AD 2012-04-08 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2012-04-10
We are adopting a new airworthiness directive (AD) for certain Model DHC-8-102, -103, and -106 airplanes and Model DHC-8-200, -300, and -400 series airplanes. This AD was prompted by reports of cracki
- TCCAEASA 2012-09 · Loss of the 400Hz Fixed Frequency System Due To Multiple Inverter Failures
Effective: 2012-02-21
- FAA AD 2012-02-12 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2012-02-15
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400, -401, and -402 airplanes. This AD requires an inspection of a certain alternating current (AC) power wi
- TCCAEASA 2012-08 · Power Lever Friction Brake Assembly Discrepancy
Effective: 2012-01-31
- TCCAEASA 2012-07 · Cockpit "Engine Fire, Check Fire Detect" Warning and "FUEL OFF" Handle Lights Failure to Reset
Effective: 2012-01-30
- TCCAEASA 2012-05 · Chafing of the Wire Harness at the Wing Leading Edge
Effective: 2012-01-18
- TCCAEASA 2012-04 · Hydraulic Accumulators - Screw Cap/End Cap Failure
Effective: 2012-01-18
- TCCAEASA 2012-03 · Electrical Power - Wire Chafing within the Alternating Current Contactor Box
Effective: 2012-01-17
- TCCAEASA 2012-02 · Rudder Control System - Seizure of the Rudder Feel Trim Unit
Effective: 2012-01-16
- TCCAEASA 2012-01 · Beta Warning Horn System Failure
Effective: 2012-01-16
- TCCAEASA 2011-46 · Burnt Alternating Current Wire Bundle Under Floor - Cockpit Door Area
Effective: 2011-12-21
- FAA AD 2011-26-05 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2012-01-23
We are superseding an existing airworthiness directive (AD) that applies to certain Bombardier, Inc. Model DHC-8-300 series airplanes. This AD results from mandatory continuing airworthiness informati
- FAA AD 2011-24-10 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2011-12-16
We are adopting a new airworthiness directive (AD) for Bombardier, Inc. Model DHC-8-201 and -202 airplanes with FAA Supplemental Type Certificate (STC) ST00753NY (Transport Canada Civil Aviation (TCCA
- FAA AD 2011-24-03 · Airworthiness Directives; Bombardier, Inc. Airplanes
Effective: 2012-01-03
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD results from mandatory continuing airworthiness information (MCAI) originated
- TCCAEASA 2011-34 · Ice Protection System - Failure of the Timer and Monitor Unit
Effective: 2011-08-26
- TCCAEASA 2011-32 · Rudder Control - Excessive Wear on the Brake Pedal Bellcrank
Effective: 2011-08-18
- TCCAEASA 2011-31 · Incorrect Heat Treatment of Pushrod Assembly
Effective: 2011-08-18
- TCCAEASA 2011-29 · Hydraulic Accumulators - Screw Cap/End Cap Failure
Effective: 2011-08-10
- TCCAEASA 2011-24 · Wing to Fuselage Attachment Joints - Barrel Nut Cracking
Effective: 2011-07-22
- TCCAEASA 2011-22 · Electrical - AC Generator Rotor Band Failure
Effective: 2011-07-19
- TCCAEASA 2011-21 · Fuel System - Chafing of High Pressure Fuel Line
Effective: 2011-07-18
- TCCAEASA 2011-20 · Power Lever Assembly - Fouling of the United Kingdom Civil Aviation Authority Flight Idle Gate
Effective: 2011-07-15
- TCCAEASA 2011-15 · Inability to Deflate the Seal and Open the Airstair Door
Effective: 2011-06-27
- TCCAEASA 2011-14 · Main Landing Gear Retraction Actuator - Retract Port Flexible Hose Failure
Effective: 2011-06-22
- TCCAEASA 2011-13 · Horizontal Stabilizer Trim - Erroneous Activation of the Take-off Configuration Aural Warning
Effective: 2011-06-15
- TCCAEASA 2011-12 · Cracked Rudder Actuator Mounting Bracket
Effective: 2011-06-09
- TCCAEASA 2011-06 · Airstair Door - Blocked Water Drainage Path
Effective: 2011-05-25
- TCCAEASA 2011-01R1 · Main Landing Gear Alternate Extension System - Cam Mechanism not in Normal Rested Position
Effective: 2011-05-20
- TCCAEASA 2011-04 · Cracking of the Outer Wing Fuel Access Panel
Effective: 2011-03-17
- TCCAEASA 2011-02 · Cargo Conversion System - Inadequate Fire Protection and Decompression Venting Means
Effective: 2011-02-03
- TCCAEASA 2011-01 · Main Landing Gear Alternate Extension System - Cam Mechanism not in Normal Rested Position
Effective: 2011-01-18
- TCCAEASA 2010-30R1 · Cracking of the Nacelle Attachment Fitting(s)
Effective: 2010-09-24
- TCCAEASA 2010-31 · Fuel System Safety - Introduction of Design Changes
Effective: 2010-09-16
- TCCAEASA 2010-30 · Cracking of the Nacelle Attachment Fitting(s)
Effective: 2010-08-31
- TCCAEASA 2010-28 · Flight Controls - Elevator Power Control Unit - Inspection / Replacement
Effective: 2010-08-24
- TCCAEASA 2010-27 · Flight Controls - Elevator Torque Tube - Replacement
Effective: 2010-08-24
- TCCAEASA 2010-26 · Landing Gear - Door Alternate Release Cable - Modification
Effective: 2010-08-23
- TCCAEASA 2010-23 · Landing Gear - Main Landing Gear (MLG) - Modification
Effective: 2010-07-23
- TCCAEASA 2010-22 · Main Landing Gear Stabilizer Extension Spring
Effective: 2010-07-22
- TCCAEASA 2010-21 · Fuel System - Inadequate Electrical Bonding of the Motive Flow Check Valve
Effective: 2010-07-22
- TCCAEASA 2010-16 · Cockpit Windshield Lower Frames - Potential for Corrosion
Effective: 2010-06-04
- TCCAEASA 2002-26R2 · Flight Controls - Flap Drive Actuator Assembly
Effective: 2010-05-10
- TCCAEASA 2009-01R1 · Dual AC Generator Shutdown
Effective: 2010-04-09
- TCCAEASA 2010-08 · Electrical Power - AC Wiring Harness Chafing on Centre Wing Lower Flap Shroud
Effective: 2010-03-22
- FAA AD 2010-04-12 · Airworthiness Directives; Bombardier, Inc. Model DHC-8-100 and DHC-8-200 Series Airplanes, and Model DHC-8-301, -311, and -315 Airplanes
Effective: 2010-04-08
We are adopting a new airworthiness directive (AD) for certain Model DHC-8-100 and DHC-8-200 series airplanes, and DHC-8-301, -311, and -315 airplanes. This AD requires implementing a corrosion preven
- TCCAEASA 2010-05 · Angle of Attack Vane - Heating Element Ageing and Resolver Oil Contamination
Effective: 2010-02-11